Implementation and Validation of a 6 Degrees-of-Freedom Nonlinear Helicopter Model
AIAA Modeling and Simulation Technologies Conference
2016-01-01
Conference paper
Electronic Resource
English
Implementation and Validation of a 6 Degrees-of-Freedom Nonlinear Helicopter Model (AIAA 2016-2139)
British Library Conference Proceedings | 2016
|Control reconfiguration demonstrated at a two-degrees-of-freedom helicopter model
British Library Conference Proceedings | 2003
|Aircraft Six-Degrees-of-Freedom Model Validation Through Flight Test
British Library Conference Proceedings | 1998
|